Application of BVF diagnosis on unsteady rotor/stator matching

Hangkong Dongli Xuebao/Journal of Aerospace Power

Volumn 22, Issue 7, 2007, Pages 1082-1086

  Rao, Jie ^a   Yuan, Wei ^a   Li, Qiu Shi ^a   Gong, Zhi Qiang ^a   Lu, Li Peng ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aerospace propulsion system; Boundary vorticity flux; Fan; Rotor stator interaction; Unsteady

Indexed keywords

PRESSURE; PROPULSION; ROTORS; VORTICITY;

AEROSPACE PROPULSION SYSTEM; BOUNDARY VORTICITY FLUX; NUMERICAL SIMULATION; ROTOR/STATOR INTERACTION; STATIC PRESSURE;

FLOW FIELDS;

EID: 34547633857     PISSN: 10008055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

1. Gallus H E, Lamberts J, Wallmann T. Blade-row interaction in an axial flow subsonic compressor state[J]. AMSE Journal of Engineering for Power, 1980, 102: 169-177.
2. Smith L Jr. Casing boundary layers in multistage axial flow compressors flow research in blading[M]. Amsterdam: I. Elsevier Publishing Company, 1970.
3. WU Jiezhi, Roach R L, Lo C F, et al. Aerodynamic diagnostics and design based on boundary vorticity dynamics[C]//17th AIAA Applied Aerodynamics Conference. AIAA-99-3103.
4. LI Qiushi. An exploration to diagnose and design for turbo-machinery based on boundary vorticity dynamics[D], Post P. H. D. Dissertation, Beijing University of Aeronautics and Astronautics. 2002. 11.
5. GUO Ming, LI Qiushi, HOU Anping, et al. A diagnostic and design approach of axial compressor based on local dynamics[R], ASME GT2006-91116.
6. Lighthill M J. Laminar boundary layer[M], Oxford: Oxford University Press, 1963: 46-113.